archive/ES_0.5598946570857316---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.00025 kN
	num_thrusters: 1
	duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-15T07:41:15.326
Launch V∞: [7.910361443980569, -5.8211127593883365, 0.09051284287402817] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.741314138835844e-9, -1.6181056957738598e-9, -2.4698750387139132e-9] km/s
	V∞_out: [-6.131056300222261e-11, 2.0072438217008642e-10, -3.239619166133486e-11] km/s
	time of flight: 1.8580091554808328e8 seconds
	arrival date: 2030-04-04T19:03:10.326
	thrust profile: [0.39300651550274873 -0.004003351417261991 -0.12252096232101974; 0.035730105417447 0.017592384488226184 -0.04338133006299266; 0.02778028484543772 0.02233977866626202 -0.05886804843546905; 0.03336958887544979 0.03789704273351734 -0.10691760973067099; 0.016421629262888 0.021743054720557084 -0.0713140558473542; 0.0188592351172839 0.030208730287002234 -0.10381401970459088; 0.01556046210861458 0.029693882879450417 -0.10716953168656726; 0.008176583952948775 0.016279059114357917 -0.06586696023982473; 0.008023162227269226 0.019413810274662196 -0.07929320161668613; 0.003440734054409636 0.008406453975348773 -0.0388028809647125; 6.410889779352507e-5 0.000798930534512131 -0.011673153193131214; -0.0008004486800498431 0.0036637614324579377 -0.0050568994961437295; 0.0019157148924420515 0.0030497170029450027 -0.002192715278606954; 0.0017160912507419527 0.002338696616854226 -0.002866558632516892; 0.00421676255973163 0.0027631294746252753 0.0030580694471102187; -0.009641032915115895 0.007535633865323639 -0.010363229818654632; -0.002267340177253321 0.002376543912596386 -0.005462170470823786; 0.005641703773325541 0.005870845614560533 -0.00838275739519161; 0.0014874644369347384 0.0015469071673322008 -0.004396636484346443; 0.004660040439796248 0.002098163105103292 -0.0023040467599910333] %

Mass Used: 90.48414031121001 kg
Launch C3: 96.46736450665318 km²/s²
||V∞_in||: 3.4279328581037696e-9 km/s